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A special method for finding body distortions that reduce the wave drag of wing and body combinations at supersonic speeds
Report presenting a consideration of the problem of shaping an adjoining fuselage for a given wing and supersonic Mach number so that the combination will have a low wave drag. Only fuselages that can be simulated by singularities distributed along the body axis are studied.
Date:
May 20, 1955
Creator:
Lomax, Harvard & Heaslet, Max A.
System:
The UNT Digital Library
Study of some effects of structural flexibility on the longitudinal motions and loads as obtained from flight measurements of a swept-wing bomber
Report presenting measurements obtained during elevator-pulse maneuvers with a Boeing B-47A airplane in the a range of Mach numbers which were analyzed to obtain frequency responses in pitching velocity and normal load factor up to frequencies of 43 radians per second.
Date:
May 20, 1955
Creator:
Donegan, James J. & Huss, Carl R.
System:
The UNT Digital Library
Effect of Several Modifications to Center Body and Cowling on Supercritical Performance of a Supersonic Inlet at Mach Number of 2.02
Report discussing an investigation of several modifications of the center body and cowling of a supersonic inlet at Mach number 2.02 and angles of attack up to 12.25 degrees. Information about the effect on stable range of boundary-layer control on the center body, the stable range of distortion of conical shock, and the stable range of cowling-lip thickness is provided.
Date:
May 20, 1955
Creator:
Trimpi, Robert L. & Cohen, Nathaniel B.
System:
The UNT Digital Library